2.75 Inch plastic warhead

• US 4,498,396 A
• Filed: 03/11/1982
• Issued: 02/12/1985
• Est. Priority Date: 03/01/1979
• Status: Expired due to Fees

• Current Assignee: Her Majesty The Queen In Right of Canada As Represented By The Minister of National Defence
• Original Assignee: Her Majesty The Queen In Right of Canada As Represented By The Minister of National Defence
• Inventors: Berube, Gilles
• Primary Examiner(s): TUDOR, HAROLD JAY
• Application Number:
  US06/357,288
• Time in Patent Office: 1,069 Days
• Field of Search: 102/501, 102/444, 102/498, 102/506, 102/529, 102/517
• US Class Current: 102/529
• CPC Class Codes: F42B 12/74 of the core or solid body
• CPC Class Codes: F42B 8/12 Projectiles or missiles F42B10/48, F42B12/36, F42B19/36 take precedence

Abstract

The invention disclosed relates to an inexpensive practice warhead for use in conjunction with combat rockets. The novel warhead is basically the same configuration and weight as conventional metal warheads, but is constructed of an inexpensive plastic material, the weight difference being made up by providing ballast means within the hollow core of the warhead.

Claims

1. A practice warhead for simulating the flight characteristics of an actual warhead, the practice warhead providing a coefficient of drag, weight and maximum cross-sectional area of the practice warhead such that the ballistic coefficient of the practice warhead matches closely that of the actual warhead, the practice warhead comprising a shell of substantially the same external configuration and maximum cross-sectional area as the actual warhead, the shell defining a hollow core, and readily insertable ballast means in the form of a cylindrical metal rod disposed in the core to provide a sufficient weight to match the ballistic coefficient of the actual warhead while maintaining flight stability, the practice warhead being characterised in that the shell is of a suitable plastic material, the cylindrical metal rod being of generally uniform diameter throughout its length, the hollow core of the shell having a forward end portion of substantially the same internal diameter as the outside diameter of the metal rod and within which said metal rod is positioned, the remainder of said hollow core being of greater diameter than said metal rod, said shell including an aft opening of greater diameter than said metal rod for receiving the metal rod within the core, a joint means detachably secured in said aft opening, said joint means being a generally cylindrical member open at one end and having a central hollow bore of the same diameter as said metal rod and within which the aft end of said metal rod is positioned whereby each end portion of the cylindrical metal rod is principally supported adjacent each of its ends and positioned to define an annular space between the metal rod and the core.

2. A practice warhead according to claim 1 further characterised in that said joint means includes external means for connecting the practice warhead to a rocket, said joint means also being of a suitable plastics material.

3. A practice warhead according to claim 1 further characterised in that said joint means is secured within said aft opening of shell by means of screw threads, said external means also comprising screw threads.

4. A practice warhead according to claim 1 or 2 or 3 further characterised by resilient spacers located between the opposing ends of the metal rod and the plastics shell and said joint means to allow for large tolerances and differential thermal expansion between the shell and the metal rod.

5. A practice warhead according to claim 1, 2 or 3, further characterised in that plastics material is a nylon/glass fibre composition comprising 60-70% by weight of nylon and 40-30% by weight of glass fibre.

6. A practice warhead according to claim 1, 2 or 3, further characterised in that the plastics material is a composition comprising 70% by weight of nylon and 30% by weight of glass fibre.